Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 89
Book Description
The report describes the theories, the numerical methods and the computer programs developed for determining the inviscid three- dimensional flow about smooth shapes at supersonic speeds. Volume 1 describes the theoretical and numerical approaches and compares two sample cases with experiment; a blunted 15 deg cone at 20 deg angle of attack in helium at M = 14. 9, and a 70 deg slab delta wing at 15 deg angle of attack in air at M = 9.6. The numerical results are in close agreement with the experimental data.
The Calculation of Three-Dimensional Supersonic Flows Around Spherically-Capped Smooth Bodies and Wings. Volume 1. Theory and Application
Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 89
Book Description
The report describes the theories, the numerical methods and the computer programs developed for determining the inviscid three- dimensional flow about smooth shapes at supersonic speeds. Volume 1 describes the theoretical and numerical approaches and compares two sample cases with experiment; a blunted 15 deg cone at 20 deg angle of attack in helium at M = 14. 9, and a 70 deg slab delta wing at 15 deg angle of attack in air at M = 9.6. The numerical results are in close agreement with the experimental data.
Publisher:
ISBN:
Category :
Languages : en
Pages : 89
Book Description
The report describes the theories, the numerical methods and the computer programs developed for determining the inviscid three- dimensional flow about smooth shapes at supersonic speeds. Volume 1 describes the theoretical and numerical approaches and compares two sample cases with experiment; a blunted 15 deg cone at 20 deg angle of attack in helium at M = 14. 9, and a 70 deg slab delta wing at 15 deg angle of attack in air at M = 9.6. The numerical results are in close agreement with the experimental data.
The Calculation of Three-dimensional Supersonic Flows Around Spherically-capped Smooth Bodies and Wings: Theory and applications
Author: Chong-Wei Chu
Publisher:
ISBN:
Category : Aerodynamics, Supersonic
Languages : en
Pages : 92
Book Description
Publisher:
ISBN:
Category : Aerodynamics, Supersonic
Languages : en
Pages : 92
Book Description
The Calculation of Three-dimensional Supersonic Flows Around Spherically-capped Smooth Bodies and Wings: Manual for computer programs
Author: Chong-Wei Chu
Publisher:
ISBN:
Category : Aerodynamics, Supersonic
Languages : en
Pages : 216
Book Description
Publisher:
ISBN:
Category : Aerodynamics, Supersonic
Languages : en
Pages : 216
Book Description
The Calculation of Three-Dimensional Supersonic Flows Around Spherically-Capped Smooth Bodies and Wings. Volume II. Manual for Computer Programs
Author: Chong-Wei Chu
Publisher:
ISBN:
Category :
Languages : en
Pages : 205
Book Description
I ;Powers, Sidney A. ;NOR-72-87-Vol-2F33615-72-C-1429AF-1366AFFDLTR-72-91-Vol-2See also Volume 1, AD-753 695.(*airframes, *supersonic characteristics), (*computer programs, aerodynamics), numerical analysis, conical bodies, delta wings, instruction manuals, blunt bodies, hypersonic characteristics, angle of attack, three dimensional flow, subroutinescomputer aided analysis, smooth bodies, inviscid flowThe report describes the theories, the numerical methods and the computer programs developed for determining the inviscid three-dimensional flow about smooth shapes at supersonic speeds. Volume II is a user's manual for the computer programs and provides the detailed information needed to set up and use the programs. These programs can determine the supersonic flow past smooth blunted bodies for any angle of attack for which the initial value surface remains on the blunted nose. The lowest usable Mach number is on the order of 2.0, with lower values attainable by careful attention to the initial value surface solution. There is no computational upper limit on the Mach number. (Author).
Publisher:
ISBN:
Category :
Languages : en
Pages : 205
Book Description
I ;Powers, Sidney A. ;NOR-72-87-Vol-2F33615-72-C-1429AF-1366AFFDLTR-72-91-Vol-2See also Volume 1, AD-753 695.(*airframes, *supersonic characteristics), (*computer programs, aerodynamics), numerical analysis, conical bodies, delta wings, instruction manuals, blunt bodies, hypersonic characteristics, angle of attack, three dimensional flow, subroutinescomputer aided analysis, smooth bodies, inviscid flowThe report describes the theories, the numerical methods and the computer programs developed for determining the inviscid three-dimensional flow about smooth shapes at supersonic speeds. Volume II is a user's manual for the computer programs and provides the detailed information needed to set up and use the programs. These programs can determine the supersonic flow past smooth blunted bodies for any angle of attack for which the initial value surface remains on the blunted nose. The lowest usable Mach number is on the order of 2.0, with lower values attainable by careful attention to the initial value surface solution. There is no computational upper limit on the Mach number. (Author).
NASA Technical Note
Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 958
Book Description
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 958
Book Description
Scientific and Technical Aerospace Reports
Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 1102
Book Description
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 1102
Book Description
STAR
Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 888
Book Description
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 888
Book Description
A Parametric Study of Effect of Forebody Shape on Flow Angularity at Mach 8
Author: Charles Borden Johnson
Publisher:
ISBN:
Category : Aerodynamics, Hypersonic
Languages : en
Pages : 52
Book Description
Publisher:
ISBN:
Category : Aerodynamics, Hypersonic
Languages : en
Pages : 52
Book Description
NASA Technical Paper
Author:
Publisher:
ISBN:
Category : Science
Languages : en
Pages : 164
Book Description
Publisher:
ISBN:
Category : Science
Languages : en
Pages : 164
Book Description
A Short Static-pressure Probe Design for Supersonic Flow
Author: Shimer Zane Pinckney
Publisher:
ISBN:
Category : Aerodynamics, Supersonic
Languages : en
Pages : 44
Book Description
Publisher:
ISBN:
Category : Aerodynamics, Supersonic
Languages : en
Pages : 44
Book Description